Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.00322569832e-12.
Allowing negative dual variable(s) as small as -5.00947503965e-12.
Allowing negative dual variable(s) as small as -4.77224986958e-12.
Allowing negative dual variable(s) as small as -1.01927815147e-11.
Solving took 4 GP solves and 1.84 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2268 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.28716566656e-12.
Allowing negative dual variable(s) as small as -4.96627912405e-12.
Allowing negative dual variable(s) as small as -4.80905853334e-12.
Allowing negative dual variable(s) as small as -1.97288899627e-11.
Solving took 4 GP solves and 1.94 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2266 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -1.61578736502e-11.
Allowing negative dual variable(s) as small as -6.10699685266e-12.
Allowing negative dual variable(s) as small as -1.1664245958e-11.
Allowing negative dual variable(s) as small as -6.61325855189e-12.
Allowing negative dual variable(s) as small as -6.58848670065e-12.
Allowing negative dual variable(s) as small as -1.10160522197e-11.
Allowing negative dual variable(s) as small as -1.16821332339e-11.
Allowing negative dual variable(s) as small as -1.10534259697e-11.
Allowing negative dual variable(s) as small as -1.11130040717e-11.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.79823523693e-11.
Allowing negative dual variable(s) as small as -6.27621392357e-12.
Allowing negative dual variable(s) as small as -1.04102257413e-11.
Allowing negative dual variable(s) as small as -1.04253627215e-11.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.91622786909e-12.
Allowing negative dual variable(s) as small as -1.28759242205e-13.
Allowing negative dual variable(s) as small as -8.82205111592e-14.
Allowing negative dual variable(s) as small as -3.22624929689e-13.
Solving took 4 GP solves and 1.95 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.91042738326e-11.
Allowing negative dual variable(s) as small as -8.92992641638e-11.
Allowing negative dual variable(s) as small as -8.98845828497e-11.
Allowing negative dual variable(s) as small as -8.47859048594e-11.
Solving took 4 GP solves and 4.79 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -1.60997257193e-11.
Allowing negative dual variable(s) as small as -6.1058172407e-12.
Allowing negative dual variable(s) as small as -1.16264151084e-11.
Allowing negative dual variable(s) as small as -6.60396737295e-12.
Allowing negative dual variable(s) as small as -6.60284327214e-12.
Allowing negative dual variable(s) as small as -1.10102415466e-11.
Allowing negative dual variable(s) as small as -1.16819245249e-11.
Allowing negative dual variable(s) as small as -1.10537822385e-11.
Allowing negative dual variable(s) as small as -1.11165437749e-11.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -1.79887762672e-11.
Allowing negative dual variable(s) as small as -6.2780063266e-12.
Allowing negative dual variable(s) as small as -1.04086779343e-11.
Allowing negative dual variable(s) as small as -1.04260413237e-11.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.91625042685e-12.
Allowing negative dual variable(s) as small as -9.38621025301e-14.
Allowing negative dual variable(s) as small as -8.84899827271e-14.
Allowing negative dual variable(s) as small as -9.0940507277e-14.
Solving took 4 GP solves and 1.85 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.90976059892e-11.
Allowing negative dual variable(s) as small as -8.93127659503e-11.
Allowing negative dual variable(s) as small as -8.98967944356e-11.
Allowing negative dual variable(s) as small as -8.47858519504e-11.
Solving took 4 GP solves and 4.98 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
